Space vehicles -- Propulsion systems
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The concept Space vehicles -- Propulsion systems represents the subject, aboutness, idea or notion of resources found in Indiana State Library.
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Space vehicles -- Propulsion systems
Resource Information
The concept Space vehicles -- Propulsion systems represents the subject, aboutness, idea or notion of resources found in Indiana State Library.
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- Space vehicles -- Propulsion systems
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- (EG-IN)644614
100+ Items that share the Concept Space vehicles -- Propulsion systems
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Context of Space vehicles -- Propulsion systemsSubject of
- 100-kW class applied-field MPD thruster component wear
- 2000-hour cyclic endurance test of a laboratory model multipropellant resistojet
- 30-kW ammonia arcjet technology : final report, July 1986-December 1989
- 8-cm ion thruster characterization
- A Two stage launch vehicle for use as an advanced space transportation system for logistics support of the space station
- A candidate architecture for monitoring and control in chemical transfer propulsion systems
- A cyclic ground test of an ion auxiliary propulsion system : description and operational considerations
- A new facility for advanced rocket propulsion research
- A two-dimensional finite difference program for thermal analysis of rocket thrust chambers
- ALS engine propellant effector system : summary final report
- Advanced APS impacts on vehicle payloads
- Advanced Engine Study program
- Advanced NSTS propulsion system verification study : final report
- Advanced beamed-energy and field propulsion concepts : final report
- Advanced chemical propulsion at NASA Lewis : metallized and high energy density propellants
- Advanced electric propulsion and space plasma contactor research
- Advanced expander test bed program
- Advanced expander test bed program : annual technical progress report, 1 Jan. - 31 Dec. 1992
- Advanced expander test bed program : preliminary design review report
- Advanced instrumentation for aeronautical propulsion research
- Advanced ion thruster research
- Advanced liquid rockets
- Advanced power sources for space missions
- Advanced propulsion concepts : 1989 JPM specialist session
- Advanced propusion for LEO and GEO platforms
- Advanced technology for future space propulsion systems
- Advanced transportation system studies : J-2S restart study final report, DR-4, Technical area 3, alternate propulsion subsystem concepts
- Advanced transportation system studies : SSME upper state use, task final report and briefing, Technical area 3, Alternate propulsion subsystem concepts
- Advanced transportation system studies : interim final report, DRs-4,8,9, Technical area 3 | Volume II, alternate propulsion subsystem concepts | final report
- Advanced transportation system studies : propulsion database task interim report, DR-4, Technical area 3, Alternate propulsion subsystem concepts
- Aeronautical propulsion--present status and future directions
- Aeropropulsion strategic plan for the 1990's : challenging the future : journey to excellence
- An assessment and validation study of nuclear reactors for low power space applications
- An evaluation of composite propulsion for single-stage-to-orbit vehicles designed for horizontal take-off
- An evaluation of metallized propellants based on vehicle performance
- An experimental investigation of two-dimensional thrust augmenting ejectors : final report, part 1
- An overview of the Lewis Research Center CSTI Thermal Management program
- Analysis of 5 KHz combustion instabilities in 40K methane/LOX combustion chambers
- Analysis of the nonvented fill of a 4.96-cubic-meter lightweight liquid hydrogen tank
- Analytical investigation of solid rocket nozzle failure
- Application of advanced computational technology to propulsion CFD
- Applying design principles to fusion reactor configurations for propulsion in space
- Arc-driven rail accelerator research : final report
- Atomic hydrogen propellants : historical perspectives and future possibilities
- Auxiliary propulsion system flight package
- Auxiliary propulsion technology for advanced earth-to orbit vehicles
- Axisymmetric single shear element combustion instability experiment
- Basic and applied research related to the technology of space energy conversion systems, 1982-1983
- Bearing tester data compilation, analysis, and reporting and bearing math modeling : final report
- Calculations of combustion response profiles and oscillations
- Combinatorial pulse position modulation for power-efficient free-space laser communications
- Comparison of a quasi-3D analysis and experimental performance for three compact radial turbines
- Comparison of dynamic isotope power systems for distributed planet surface applications
- Comparison of thermal analytic model with experimental test results for 30-centimeter-diameter engineering model mercury ion thruster
- Computer code for single-point thermodynamic analysis of hydrogen/oxygen expander-cycle rocket engines
- Concept for a power system controller for large space electrical power systems
- Cycle 0(CY1991) NLS trade studies and analyses report
- Cyclic structural analyses of anisotropic turbine blades for reusable space propulsion systems
- Design and analysis report for the flight weight 20-inch Columbium secondary nozzle for the RL10 engine
- Design and demonstrate the performance of cryogenic components representative of space vehicles : start basket liquid acquisition device performance analysis
- Design and demonstration of a system for the deposition of atomic-oxygen durable coatings for reflective solar dynamic power system concentrators
- Design considerations for space radiators based on the liquid sheet (LSR) concept
- Design of a solar sail mission to Mars
- Design optimization of gas generator hybrid propulsion boosters
- Design verification test matrix development for the STME thrust chamber assembly
- Development and flight history of SERT II spacecraft
- Development of a liquid-fed water resistojet
- Development of advanced seals for space propulsion turbomachinery
- Development of arcjet anf ion propulsion for spacecraft stationkeeping
- Effect of anisotropic conduction and heat pipe interaction on minimum mass space radiators
- Effects of dust accumulation and removal on radiator services on Mars
- Effects of propulsion system characteristics on ascent performance of dual-fueled single-stage earth-to-orbit transports
- Electromagnetic propulsion for spacecraft
- Elements of propulsion
- Emergency egress fixed rocket package : patent application
- Energy efficient engine flight propulsion system preliminary analysis and design report : final update
- Environmental interactions and the SP-100 power system
- Evaluation of advanced propulsion options for the next manned transportation system : propulsion evolution study : final report
- Experimentation in the low-density plume of a simulated electrothermal thruster for computer code validation
- Extended temperature range rocket injection : patent application
- Feasibility study of LITVC for Shuttle SRB
- Fiberoptics for propulsion control systems
- Filament wound metal lined propellant tanks for future earth-to-orbit transports
- Final report, space shuttle main engine structural analysis and data reduction/evaluation, Volume 3A, High pressure oxidizer turbo-pump preburner pump housing stress analysis report
- Flight motor set 360L001 (STS-26R) : final report (reconstructed dynamic loads analysis)
- Flight motor set 360L001 (STS-26R) : final report, Volume 5, Nozzle component
- Flight motor set 360L001 (STS-26R), final report, Volume 1
- Flight motor set 360L001 (STS-26R), final report, Volume I
- Flight set 360L001 (STS-26) igniter, post flight, final report, Volume 6
- Fusion energy for space : feasiblity demonstration : a proposal to NASA
- Fusion energy for space missions in the 21st century
- Fuzzy logic approaches to multi-objective decision-making in aerospace applications
- Heat transfer in aeropropulsion systems
- Heat transfer in aerospace propulsion
- Heaterless ignition of inert gas ion thruster hollow cathodes
- High efficiency direct thermal to electric energy conversion from radioisotope decay using selective emitters and spectrally tuned solar cells
- High heat transfer oxidizer heat exchanger design and analysis : final report, Jan. 1985 - Oct. 1986
- High power ion thruster performance
- High temperature thruster technology for spacecraft propulsion
- High- and low-thrust propulsion systems for the space station
- Hybrid propulsion technology program : final report
- Hybrid propulsion technology program : final report, Volume IV
- Hybrid propulsion technology program : phase I, final report
- Hybrid propulsion technology program, phase I : final report
- Hydrogen/oxygen auxiliary propulsion technology
- Identification of propulsion systems
- Identification of space shuttle main engine dynamics
- Igniter heater EMI transient test : final report
- Ignition characterization of LOX/hydrocarbon propellants : final report
- Ignition characterization of LOX/hydrocarbon propellants : final summary report
- Integrated controls and health monitoring for chemical transfer propulsion
- Integrated model development for liquid fueled rocket propulsion systems
- Internal ballistics model update for ASRM dome : final technical report for the period August 31, 1990 through February 20, 1991
- Internal erosion rates of a 10-kW xenon ion thruster
- Interstellar propulsion using a pellet stream for momentum transfer
- Ion propulsion for spacecraft
- Large Space Systems/Low-Thrust Propulsion Technology : an Industry-Government information exchange
- Large liquid rocket engine transient performance simulation system
- Large liquid rocket engine transient performance simulation system : final report
- Large scale advanced prop-fan (LAP) static rotor test report
- Leakage predictions for Rayleigh-step, helium-purge seals
- Liquid Rocket Booster (LRB) for the Space Transportation System (STS) systems study, Volume II, Final report, addendum 2
- Liquid rocket booster study : addendum to final report
- Liquid rocket booster study : final report, Volume I, Executive summary
- Liquid rocket booster study : final report, Volume II | Appendices 2-5, PIPP, transition plan, Amos plan environmental analysis
- Liquid rocket booster study : final report, Volume II | Appendices 2-5, PPIP, transition plan, AMOS plan, environmental analysis
- Liquid rocket booster study : final report, Volume II | Appendices 6-8, Final reports of Rocketdyne, Pratt and Whitney, and TRW
- Liquid rocket booster study : final report, Volume II | Appendix 10, Eagle engineering | Final report
- Liquid rocket booster study : final report, Volume II | Appendix I, Trades studies
- Liquid rocket booster study : final report, Volume II, Final report
- Liquid rocket booster study, Volume II | Appendix 9 | Book 5, LRB alternate applications and evolutionary growth
- Literature concerning control and display technology applicable to the Orbital Maneuvering Vehicle (OMV)
- Low earth durability evaluation of protected silicone for advanced refractive photovoltaic concentrator arrays
- Low earth orbital atomic oxygen environmental simulation facility for space materials evaluation
- Low power arcjet performance
- Low thrust chemical rocket technology
- Lunar lander and return propulsion system trade study
- Mach 6.5 air induction system design for the Beta II two-stage-to-orbit booster vehicle
- Main propulsion system test requirements for the two-engine shuttle-C
- Manrating orbital transfer vehicle propulsion
- Mass study for modular approaches to a solar electric propulsion module
- Medium power hydrogen arcjet performance
- Microgravity liquid propellant : final report
- Mirror fusion propulsion system : a performance comparison with alternate propulsion systems for the manned Mars mission
- Modification of NASA Langley 8-foot high temperature tunnel to provide a unique national research facility for hypersonic air-breathing propulsion systems
- Multi-disciplinary coupling effects for integrated design of propulsion systems
- NASA directions in space propulsion for 2000 and beyond
- NASA requirements and applications environments for electrical power wiring
- Neutralizer optimization
- New method of making advanced tube-bundle rocket thrust chambers
- Nondestructive evaluation tools and experimental studies for monitoring the health of space propulsion systems
- Nuclear powered Mars cargo transport mission utilizing advanced ion propulsion
- Numerical investigations in the backflow region of a vacuum plume : semi-annual scientific and technical reports, October 1991 - May 1992
- Options for thrust augmentation for the Beta II two-stage-to-orbit launch vehicle
- Orbital maneuvering vehicle (OMV) : plume and plume effects study : final report
- Orbital transfer vehicle 3000 lbF thrust chamber assembly hot-fire test program : interim report
- Orbital transfer vehicle engine technology : baffled injector design, fabrication and verification
- Overview of free-piston Stirling SP-100 activities at the NASA Lewis Research Center
- Performance and heat transfer characteristics of a carbon monoxide/oxygen rocket engine
- Performance assessment of low pressure nuclear thermal propulsion
- Performance characteristics of ring-cusp thrusters with xenon propellant
- Performance of 10-kW class xenon ion thrusters
- Performance of large area xenon ion thrusters for orbit transfer missions
- Plans for the development of cryogenic engines for space exploration
- Plug nozzles--the ultimate customer driven propulsion system
- Power generation technology options for a Mars mission
- Power transmission by laser beam from lunar-synchronous satellite
- Preliminary SP-100/Stirling heat exchanger designs
- Preliminary base heating environments for a generalized ALS LO2/LH2 launch vehicle : [appendix 1 and 2]
- Preliminary characterization of a water vaporizer for resistojet applications
- Preliminary designs for 25 kWe advanced Stirling conversion systems for dish electric applications
- Preliminary development of an intelligent computer assistant for engine monitoring
- Preliminary engineering report for design of a subscale ejector/diffuser system for high expansion ratio space engine testing
- Preliminary performance characterizations of an engineering model multipropellant resistojet for space station application
- Prioritization methodology for chemical replacement
- Probability of failure and risk assessment of propulsion structural components
- Process comparison study : MSFC center director's discretionary fund final report (Project number 89-03)
- Project Argo : the design and analysis of an all-propulsive and an aeroassisted version of a manned space transportation vehicle
- Propulsion issues for advanced orbit transfer vehicles
- Propulsion systems using in situ propellants for a Mars ascent vehicle
- Proven, long-life hydrogen/oxygen thrust chambers for space station propulsion
- Purging of multilayer insulation by gas diffusion
- RSRM-3 (360L003) : final report : ballistics/mass properties
- RSRM-4 (360T004) : final report : ballistics/mass properties
- Radiation resistance of thin-film solar cells for space photovoltaic power
- Rail accelerators for space transportation : an experimental investigation
- Real-time fault diagnosis for propulsion systems
- Recent advances in low-thrust propulsion technology
- Reliability studies of Integrated modular engine system designs
- Research pressure instrumentation for NASA space shuttle main engine : monthly report
- Resistojet control and power for high frequency ac buses
- Resistojet plume and induced environment analysis
- Resistojet propulsion for large spacecraft systems
- Review of advanced radiator technologies for spacecraft power systems and space thermal control
- SEI power source alternatives for rovers and other multi-kWe distributed surface applications
- SRB/SLEEC (Solid Rocket Booster/Shingle Lap Extendible Exit Cone) feasibility study : final report, Volume 1
- SRB/SLEEC (Solid Rocket Booster/Shingle Lap Extendible Exit Cone) feasibility study : final report, Volume 2 | Appendix A, Design study for a SLEEC actuation system
- Slush hydrogen (SLH2) technology development for application to the National Aerospace Plane (NASP)
- Small hydrogen/oxygen rocket flowfield behavior from heat flux measurements
- Solar electric propulsion for Mars transport vehicles
- Solar-electric-propulsion cargo vehicles for split/sprint Mars mission
- Space Station Propulsion Technology : second annual progress report
- Space chemical propulsion test facilities at NASA Lewis Research Center
- Space shuttle main engine structural analysis and data reduction/evaluation : final report, Volume 6, Primary nozzle diffuser analysis
- Space shuttle technical evaluation motor no. 3 (ITEM-3) : final test report
- Space station propulsion analysis study
- Space station propulsion requirements study
- Space station propulsion technology first annual progress report
- Space station propulsion test bed
- Stationary plasma thruster plume characteristics
- Stationary plasma thruster plume emissions
- Status of 20 kHz space station power distribution technology
- Status of advanced orbital transfer propulsion
- Structural dynamic measurement practices for turbomachinery at the NASA Lewis Research Center
- Structural integrity and durability for space shuttle main engine and future reusable space propulsion systems
- Structurally compliant rocket engine combustion chamber : experimental and analytical validation
- Study of auxiliary propulsion requirements for large space systems
- Study of basic physical processes in liquid and solid rocket propulsion : final technical report ...
- Technology issues associated with fueling the National Aerospace Plane with slush hydrogen
- Technology issues associated with using densified hydrogen for space vehicles
- Technology requirements for advanced earth-orbital transportation systems , duel-mode propulsion
- The Pathfinder chemical transfer propulsion program
- The chemical effects of the Martian environment on power system component materials : a theoretical approach
- The fault monitoring & diagnosis knowledge-based system for space power systems : AMPERES (NAG8-721) : phase I final report
- The large area pulsed solar simulator (LAPSS)
- The mechanisms of flame holding in the wake of a bluff body : final report NASA grant NAG 3-60, May 21, 1980 to August 21, 1983
- The preliminary checkout, evaluation and calibration of a 3-component force measurement system for calibrating propulsion simulators for wind tunnel models
- Thermal Storage Advanced Thruster System (TSATS) experimental program
- Thermal storage advanced thruster system (TSATS) experimental program : final report
- Three dimensional thermal analysis of rocket thrust chambers
- Transpiration cooled throat for hydrocarbon rocket engines : final report
- Turbine rotor/stator plowfield analysis
- Variable speed induction motor operation from a 20-kHz power bus
- Verification of thermal analysis codes for modeling sold rocket nozzles
- Water-propellant resistojets for man-tended platforms
- [A conceptual design of an unmanned test vehicle using an airbreathing propulsion system]
- [Advanced expander test engine] : [annual technical progress report, no. 2, 1 Jan. - 31 Dec. 1992]
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<div class="citation" vocab="http://schema.org/"><i class="fa fa-external-link-square fa-fw"></i> Data from <span resource="http://link.library.in.gov/resource/KwHgoj5oqP0/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.library.in.gov/resource/KwHgoj5oqP0/">Space vehicles -- Propulsion systems</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.library.in.gov/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.library.in.gov/">Indiana State Library</a></span></span></span></span></div>
